4-4. Show your complete solution. A cantilever beam ABCDE is loaded as shown. If the flexural rigidity is 5 kN:m?, determine thefollowing using the double integration method:a. The general moment equation, M (section the beamat its rightmost segment; a 50% penalty will begiven to those who will not follow this instruction)b. The slope equation of the beam, Elec. The deflection equation of the beam, Elyd. The deflection at the middle of the beamUe. The elastic curve of the beam. Create a table Ashowing the values of the slope, 0 (in degrees), anddeflection y (in mm), at points A, B, C, D, and E of thebeam. Plot these points to generate the elastic curve.M+im-2 m2 m1 mM = 16 NmU = 40 N/mW = 80 N/m

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A cantilever beam ABCDE is loaded as shown. If the flexural rigidity is 5 kN-m?, determine the following using the double integration method: a. The general moment equation, M (section the beam at its rightmost segment; a 50% penalty will be given to those who will not follow this instruction) b. The slope equation of the beam, EIO c. The deflection equation of the beam, Ely d. The deflection at the middle of the beam DE e. The elastic curve of the beam. Create a table A showing the values of the slope, 0 (in degrees), and deflection y (in mm), at points A, B, C, D, and E of the beam. Plot these points to generate the elastic curve. M 1m+ 2 m 1m M = 16 Nm U = 40 N/m W = 80 N/m

A cantilever beam ABCDE is loaded as shown. If the flexural rigidity is 5 kN-m?, determine the following using the double integration method: a. The general moment equation, M (section the beam at its rightmost segment; a 50% penalty will be given to those who will not follow this instruction) b. The slope equation of the beam, EIO c. The deflection equation of the beam, Ely d. The deflection at the middle of the beam DE e. The elastic curve of the beam. Create a table A showing the values of the slope, 0 (in degrees), and deflection y (in mm), at points A, B, C, D, and E of the beam. Plot these points to generate the elastic curve. M 1m+ 2 m 1m M = 16 Nm U = 40 N/m W = 80 N/m

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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